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bineet_aero June 12, 2016 14:46

Pressure Outlet BC
 
Hello,

For a incompressible flow case( simple channel flow), i took BC of inlet as velocity inlet, u = cont, v =w =0.

For outlet, BC is pressure outlet, static pressure 0. My question is for outlet how the BCs for u v w are treated ? Is it delu/delx = delv/delx = delw/delx = 0 ?

Thanks

FMDenaro June 12, 2016 14:57

fixing at the outlet a homogeneous Neuman bc.s as numerical condition for the velocities is acceptable for low Re flows where you can suppose no further relevance in the velocity variation. However, the outlet must be enough far to let the two boundary layer developping and create a fully developed flow.

bineet_aero June 12, 2016 15:01

Hello Mr FMDenaro,

Thanks for your reply. The simulations are for laminar regime.

Regards

FMDenaro June 12, 2016 15:07

Quote:

Originally Posted by bineet_aero (Post 604506)
Hello Mr FMDenaro,

Thanks for your reply. The simulations are for laminar regime.

Regards


starting with the plug profile at inlet you need to have a sufficient streamwise lenght to let the flow developping fully


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